About: Akaflieg Braunschweig SB-8

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The Akaflieg Braunschweig SB-8 is an experimental, single-seat, high performance glider built in Germany in the 1960s, constructed largely from glass fibre skin over built up balsa wood structure. Two were built; the second of which was later fitted with a high aspect ratio (30:1) wing, becoming the Akaflieg Braunschweig SB-9 Stratus.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	Akaflieg Braunschweig SB 8 (de) Akaflieg Braunschweig SB-8 (en)
rdfs:comment	Die SB 8 ist ein einsitziges Segelflugzeug der Akaflieg Braunschweig. Der Erstflug erfolgte am 25. April 1967 auf dem Flughafen Braunschweig. (de) The Akaflieg Braunschweig SB-8 is an experimental, single-seat, high performance glider built in Germany in the 1960s, constructed largely from glass fibre skin over built up balsa wood structure. Two were built; the second of which was later fitted with a high aspect ratio (30:1) wing, becoming the Akaflieg Braunschweig SB-9 Stratus. (en)
dcterms:subject	1960s German experimental aircraft 1960s German sailplanes Akaflieg Braunschweig aircraft Shoulder-wing aircraft Aircraft first flown in 1967
Wikipage page ID	36480662 (xsd:integer)
Wikipage revision ID	1117634000 (xsd:integer)
Link from a Wikipage to another Wikipage	Balsa Elevator (aircraft) Germany Shoulder wing Plywood Aileron West Germany Leading edge Ailerons Aircraft fabric covering Akaflieg Braunschweig SB-10 Schirokko Akaflieg Braunschweig SB-7 Nimbus 1960s German experimental aircraft 1960s German sailplanes Akaflieg Braunschweig aircraft Glider (sailplane) HKS-1 Flap (aircraft) Shoulder-wing aircraft Aeroelasticity Aircraft first flown in 1967 Chord (aircraft) Landing gear Tailplane Air brake (aircraft) Aspect ratio (wing) Canopy (aircraft) Rudder Experimental aircraft Dihedral (aircraft) Wing loading Schempp-Hirth Nimbus Flaperon T-tail dbr:Akaflieg_Braunschweig Glass fibre Glass reinforced plastic dbr:Akaflieg_Braunschweig_SB-6 dbr:Wortmann_FX_62
sameAs	Akaflieg Braunschweig SB-8 Akaflieg Braunschweig SB-8 Akaflieg Braunschweig SB-8 Akaflieg Braunschweig SB-8
sink rate ms	0.610000 (xsd:double)
sink rate note	::::SB-9: at at and (en) at at and (en)
span m	18 (xsd:integer)
span note	::::SB-9: (en)
wing area note	::::SB-9: (en)
wing area sqm	14.100000 (xsd:double)
wing loading kg/m	28.600000 (xsd:double)
wing loading note	::::SB-9: maximum wing loading (en)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Short_description dbt:Aircraft_specs dbt:Infobox_Aircraft_Type dbt:Akaflieg_Braunschweig_aircraft
dbp:primeUnits%3F_	met (en)
first flight	1967 (xsd:integer)
national origin	West Germany
crew	1 (xsd:integer)
type	Single seat experimental glider (en)
has abstract	Die SB 8 ist ein einsitziges Segelflugzeug der Akaflieg Braunschweig. Der Erstflug erfolgte am 25. April 1967 auf dem Flughafen Braunschweig. (de) The Akaflieg Braunschweig SB-8 is an experimental, single-seat, high performance glider built in Germany in the 1960s, constructed largely from glass fibre skin over built up balsa wood structure. Two were built; the second of which was later fitted with a high aspect ratio (30:1) wing, becoming the Akaflieg Braunschweig SB-9 Stratus. (en)
airfoil	root:Wortmann FX 62-K-153, mid:Wortmann FX 62-K-131, tip:Wortmann FX 60-126 (en)
aspect ratio	23 (xsd:integer) ::::SB-9: 31.3 (en)
developed from	Akaflieg Braunschweig SB-7 Nimbus
developed into	Akaflieg Braunschweig SB-10 Schirokko
empty weight kg	301 (xsd:integer)
empty weight note	::::SB-9: (en)
glide ratio	41.600000 (xsd:double)
gross weight kg	403 (xsd:integer)
length m	7.505000 (xsd:double)

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